TURBOJET NACELLE Russian patent published in 2015 - IPC B64D29/06 

Abstract RU 2569503 C2

FIELD: aircraft engineering.

SUBSTANCE: claimed nacelle comprises air intake, mid and rear sections. Mid section is composed of airframe that makes the nacelle outer aerodynamic integrity. Said airframe is rigidly jointed the adjoining fixed structure and can be detached therefrom.

EFFECT: decreased weight of nacelle components.

11 cl, 6 dwg

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RU 2 569 503 C2

Authors

Hurlin Herve

Dezeustre Nicolas

Kerbler Olivier

Gallet Francois

Desjoyeaux Bertrand

Dates

2015-11-27Published

2011-06-17Filed